2 Paganucci F, Agostini M, Andrenucci M, et al. Further experimental evidences of the development of kink insta-bilities in MPD Thrusters. AIAA-2005-4249, 2005
[3]
3 Resler EL, Sears WR. The prospects for magnetoaerody-namics. Journal of the Aeronautical Sciences, 1958, 25(4):235-245
[4]
4 Macheret SO, Miles RB. Feasibility study of a hybrid MHD/radiativily driven facility for hypersonic ground test-ing. AIAA-1997-2429, 1997
[5]
5 Gurijanov EP, Harsha PT. AJAX: New directions in hy-personic technology. AIAA-1996-4609, 1996
[6]
6 苏纬仪,张新宇,张堃元. 洛伦兹力控制高超声速进气道边界层 分离的数值模拟. 推进技术,2011, 32(1): 36-41 (Su Weiyi, Zhang Xinyu, Zhang Kunyuan. Numerical investigation of Lorentz force control on hypersonic inlet boundary layer separation. Journal of Propulsion Technology, 2011, 32(1):36-41 ( in Chinese ))
[7]
7 Macheret SO. Physics of magnetically accelerated non-equilibrium surface discharge in high-speed flow. AIAA-2006-1005, 2006
[8]
8 Kalra C, Zaidi SH, Alderman BJ, et al. Non-thermal con-trol of shock-wave induced boundary layer separation using magneto-hydro-dynamics. AIAA-2007-4138, 2007
[9]
9 Pate SR, Sile LG, Stallings DW, et al. Development of an MHD-augmented, high enthalpy, shock tunnel facility. AIAA Journal, 1974, 12(3): 289-297
[10]
10 David WB, Unmeel BM. Experimental demonstration of Magneto-Hydro-Dynamics (MHD) acceleration. AIAA-2003-4285, 2003
[11]
11 Asano H, Kaminaga S, Yamasaki H. Effect of non-uniform discharge on performance of MHD accelerator with non-equilibrium plasma. AIAA-2006-969, 2006
[12]
12 Harada N. MHD acceleration studies at Nagaoka Univer-sity of Technology. AIAA-2001-2744, 2001
[13]
13 Harada N, Ikewada J, Terasaki Y. Basic studies on an MHD accelerator. AIAA-2002-2175, 2002
[14]
14 Harada N, Kubo A, Ishizuka H, et al. Experiments for pulsed MHD accelerator driven by model rocket engine. AIAA-2010-4305, 2010
[15]
15 Macheret SO, Shneider MN, Miles RB. Electron beam gen-erated plasmas in hypersonic MHD channels. AIAA-1999-3635, 1999
[16]
16 Macheret SO, Shneider MN, Miles RB. External supersonic flow and scramjet inlet control by MHD with electron beam ionization. AIAA-2001-0492, 2001
[17]
17 Macheret SO, Shneider MN, Miles RB. Optimum perfor-mance of electron beam driven magnetohydrodynamic gen-erators for scramjet inlet control. AIAA Journal, 2007,45(9): 2157-2163
[18]
18 Macheret SO, Shneider MN, Miles RB, et al. Electron-beam-generated plasmas in hypersonic magnetohydrody-namic channels. AIAA Journal, 2001, 39(6): 1127-1138
[19]
19 Macheret SO, Shneider MN, Miles RB. Magnetohydrody-namic control of hypersonic flows and scramjet inlets using electron beam ionization. AIAA Journal, 2002, 40(1): 74-81.
[20]
20 Nishihara M, Jang NB, Lemper WR, et al. MHD super-sonic boundary layer control using pulsed discharge ioniza-tion. AIAA-2005-1341, 2005
[21]
21 Nishihara M, Jiang NB, Rich JW, et al. Low-temperature supersonic boundary layer control using repetitively pulsed MHD forcing. AIAA-2005-5178, 2005
[22]
22 Nishihara M, Rich JW, Lempert WR, et al. Low-temperature M = 3 flow deceleration by Lorentz force. Physics of Fluids, 2006, 18(8): 1-11
[23]
23 Nishihara M, Bruzzese J, Adamovich IV. Experimental and computational studies of low-temperature M = 4 flow de-celeration by Lorentz force. AIAA-2007-4595, 2007
[24]
24 Shibkov VM, Abramova AD, Chernikov AV, et al. Mi-crowave discharges in supersonic plasma aerodynamics. AIAA-2004-513, 2004
[25]
25 Litchford RJ, Cole JW, Lineberry JT, et al. Magnetohy-drodynamic augmented propulsion experiment: I. Perfor-mance analysis and design. AIAA-2002-2184, 2002
[26]
26 王永寿,陈延辉. 电磁流体力学技术在航空航天领域的应用. 飞航导弹2009, (3): 11-16 (Wang Yongshou, Chen Yan-hui. Application of magnetohydrodynamics technology in aerospace field. Winged Missiles Journal, 2009, (3): 11-16 ( in Chinese))
[27]
27 Girgis IG, Brown GL, Miles RB. Fluid mechanics of a Mach7-12, electron-beam driven, missile-scale hypersonic wind tunnel: Modeling and predictions. Physics of Fluids, 2002,14(11): 4026-4039
[28]
28 Blankson IM, Schneider S. Hypersonic engine using MHD energy bypass with a conventional turbojet. AIAA-2003-6922, 2003
[29]
29 Adamovich IV, William RJ, Schneider SJ, et al. Magne-togasdynamic power extraction and flow conditioning for a gas turbine. AIAA-2003-4289, 2003
31 Parent B, Macheret S, Shneider M, et al. Numerical study of an ebeam-confined Faraday accelerator. AIAA-2006-2890, 2890
[32]
32 Takeshita S, Buttapeng C, Harada N. Characteristics of plasma produced by MHD technology and its application to propulsion systems. Vacuum, 2010, 84(5): 685-688
[33]
33 于达仁,唐井峰,鲍文. 用于高超声速推进的MHD-Arc-Ramjet 联合循环. 航空学报, 2007, 28(4): 769-775 (Yu Daren, Tang Jingfeng, Bao Wen. MHD-Arc-Ramjet com-bined cycle for hypersonic propulsion. Acta Aeronautica et Astronautica Sinica, 2007, 28(4): 769-775 (in Chinese))
[34]
34 于达仁,唐井峰,鲍文. 多电弧对MHD-Arc-Ramjet 联合循 环发动机性能的影响. 推进技术, 2008, 29(6): 759-763 (Yu Daren, Tang Jingfeng, Bao Wen. Effects of multi-stage arc on the performance of MHD-Arc-Ramjet combined cy-cle engine. Journal of Propulsion Technology, 2008, 29(6):759-763 (in Chinese))
[35]
35 Tang JF, Bao W, Yu DR. The influence of energy-bypass on the performance of AJAX. AIAA-2006-1376, 2006
[36]
36 郑小梅. 高超声速飞行器磁流体技术数值模拟研究. [博士论文]. 北京:北京航空航天大学,2009 (Zheng Xiaomei. Numerical investigation of the MHD technology in hypersonic vehicle application. [PhD Thesis]. Beijing: Beijing University of Aeronautics and Astronautics, 2009 (in Chinese))
[37]
37 张康平,田正雨,冯定华等. 三维磁流体动力学管道流动加减速 控制数值研究. 空气动力学报, 2009, 27(4): 474-479 (Zhang Kangping, Tian Zhengyu, Feng Dinghua, et al. Numer-ical study of acceleration/deceleration control of three-dimensional magnetohydrodynamic flow in channel. Acta Aerodynamica Sinica, 2009, 27(4): 474-479 (in Chinese))
[38]
38 李益文,李应红,张百灵等. 基于激波风洞的超声速磁流体动力 技术实验系统. 航空学报,2011, 32(6): 1015-1024 (Li Yiwen, Li Yinghong, Zhang Bailing, et al. Supersonic magnetohy-drodynamic technical experimental system based on shock tunnel. Acta Aeronautical et Astronautica Sinica, 2011,32(6): 1015-1024 (in Chinese))
[39]
39 李益文,李应红,张百灵等. 超声速气流磁流体加速初步实 验研究. 力学学报,2012, 44(2): 238-244 (Li Yingwen, Li Yinghong, Zhang Bailing, et al. Preliminary experimen-tal investigation on supersonic flow magnetohydrodynamic (MHD) acceleration. Chinese Journal of Theoretical and Applied Mechanics, 2012, 44(2): 238-244 (in Chinese))
[40]
40 李益文. 高超声速飞行磁流体动力技术原理研究. [博士论文]. 西安:空军工程大学,2011 (Li Yiwen. Theory investigation of the MHD dynamic technology in hypersonic flight. [PhD Thesis]. Xi'an: Airforce Engineering University, 2011 (in Chinese))
[41]
41 Robert CM, Sohail HZ, Mikhail NS, et al. Non-equilibrium innization techniques for MHD power extraction in high-speed flows. AIAA-2003-1049, 2003
[42]
42 Itoh K, Ishikawa M. Three-dimensional analyses of phe-nomena near anode of MHD generator with high temper-ature, high velocity, and strong MHD interaction. AIAA-2001-2810, 2001
[43]
43 Macheret SO, Shneider MN, Murray RC, et al. RD-HWT/MARIAH II MHD modeling and experiments re-view. AIAA-2004-2485, 2004
